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    Title :

    Effect of Initial Flight Path Angle Error and Control Constraint on the Optimized Ascent Trajectory of a Typical Launch Vehicle


    Contributors:

    Conference:

    19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Publication date :

    2014-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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